Updated antenna positions

I had previously planned the antenna positions both disconsidering convenience of mounting the antennas, and assuming I'd have the MotoPOD on the bottom. Given this, I took some time to re-plan their placement taking both into consideration (click on any of these for a larger version - original file here). In these drawings, the solid circles are the ideal ground planes, and other circles are additional restrictions.

Top view - ELT, Stormscope, COM, GPS and TAS antennas
I no longer need separate UAT and transponder antennas. Given that Garmin requires a minimum of 3' of cable from the transponder to the antenna, I moved that antenna to the rear part of the tailcone:

Side view with all antennas

Bottom view - transponder, COM, NAV and TAS antennas

I added a third GPS antenna - one for the GTN, one GPS+XM for the G3X (PFD only), and one for the G5.

TAS antenna details - ideal and minimum ground plane plus distance to other antennas
I moved the bottom TAS antenna to inside the forward tunnel, since the aft part of the tunnel has no easy way to run cables to it, and very little clearance near the skin, with the elevator pushrod going through it. The distance between the top and bottom antennas is about 21", which should add a bearing error of about 0.2˚ for a target at 1 mile (perfectly acceptable, I doubt the TAS has that level of precision anyway):

Distance between the two TAS antennas - this introduces ~0.2˚ bearing error for a 9 or 3 o'clock target at 1sm

With the transponder antenna moved aft, I'll try using the original XPDR antenna hole for my bottom COM antenna. It's unclear what kind of performance I can get from the ground plane at that location, but since the ground plane area is only about 20% smaller than the top antenna's, I'll just plot the VSWR after the tailcone is attached and see (and if that doesn't work, I'll add another hole in the baggage area and plug this one).

COM ground plane area is ~1371sqin (ideal is ~1662sqin, ~20% more)
I was also briefly worried that the tailcone antennas might be too close to the ground in a maximum takeoff rotation position, but a quick measurement showed that's not the case (i.e. the tail would hit the ground first):

Tailcone antenna ground clearance at maximum rotation attitude

Given that none of these require any structural changes for now (only the top TAS antenna will give me trouble), I'm deferring any installation steps to later when I actually have the avionics - who knows what else may change until then.

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